P
US10975718B2ActiveUtilityPatentIndex 53

Stainless steel alloys, turbocharger turbine housings formed from the stainless steel alloys, and methods for manufacturing the same

Assignee: HONEYWELL INT INCPriority: Feb 12, 2013Filed: Feb 12, 2013Granted: Apr 13, 2021
Est. expiryFeb 12, 2033(~6.6 yrs left)· nominal 20-yr term from priority
Inventors:CHINTALAPATI PAVANNANDAGOPAL BALASUBRAMANIGURUPRASANNA PRAVEENWILSON MARCPATIL VIJAYMAHANTESHLAISSUS JEAN-JACQUES
C22C 38/02C22C 38/48C22C 38/58F01D 25/005C22C 38/44F01D 25/24F05D 2220/40F02C 6/12C22C 38/34Y10T29/49229F01D 25/00
53
PatentIndex Score
0
Cited by
44
References
14
Claims

Abstract

Disclosed is an austenitic stainless steel alloy that includes, by weight, about 16% to about 21% chromium, about 4.5% to about 5.5% nickel, about 2% to about 5% manganese, about 1% to about 2% silicon, about 0.8% to about 1.2% tungsten, about 0.4% to about 0.8% molybdenum, about 0.4% to about 0.6% niobium, about 0.4% to about 0.5% carbon, and a balance of iron. The alloy is suitable for use in turbocharger turbine housing applications for temperature up to about 1020° C.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
       1. An austenitic stainless steel alloy, comprising, by weight:
 about 16% to about 21% chromium; 
 about 4.5% to about 5.5% nickel; 
 3% to 4% manganese; 
 1.3% to 1.7% silicon; 
 about 0.8% to about 1.2% tungsten; 
 0.5% to 0.7% molybdenum; 
 0.45% to 0.55% niobium; 
 about 0.4% to about 0.5% carbon; 
 about 0.03% phosphorous or less; 
 about 0.03% sulfur or less; 
 about 0.01 to about 0.15% nitrogen; and 
 a balance of iron and unavoidable impurities. 
 
     
     
       2. The austenitic stainless steel alloy of  claim 1  comprising about 18% to about 19% chromium. 
     
     
       3. The austenitic stainless steel alloy of  claim 1  comprising about 4.7% to about 5.3% nickel. 
     
     
       4. The austenitic stainless steel alloy of  claim 1  comprising about 0.9% to about 1.1% tungsten. 
     
     
       5. The austenitic stainless steel alloy of  claim 1  comprising about 0.43% to about 0.47% carbon. 
     
     
       6. The austenitic stainless steel alloy of  claim 1 , wherein the austenitic stainless steel alloy further comprises an amount of at least one of boron, calcium, and cerium, wherein said amount, with respect to each such element so-included, is less than about 0.005%. 
     
     
       7. The austenitic stainless steel alloy of  claim 1 , wherein the austenitic stainless steel alloy further comprises an amount of at least two of boron, calcium, and cerium, wherein said amount, with respect to each such element so-included, is less than about 0.005%. 
     
     
       8. The austenitic stainless steel alloy of  claim 1 , wherein the austenitic stainless steel alloy further comprises boron, calcium, and cerium, wherein said amount, with respect to each such element, is less than about 0.005%. 
     
     
       9. An turbocharger turbine housing comprising:
 an austenitic stainless steel alloy, wherein the austenitic stainless steel alloy comprises, by weight: 
 about 16% to about 21% chromium; 
 about 4.5% to about 5.5% nickel; 
 3% to 4% manganese; 
 1.3% to 1.7% silicon; 
 about 0.8% to about 1.2% tungsten; 
 0.5% to 0.7% molybdenum; 
 0.45% to 0.55% niobium; 
 about 0.4% to about 0.5% carbon; 
 about 0.03% phosphorous or less; 
 about 0.03% sulfur or less; 
 about 0.01 to about 0.15% nitrogen; and 
 a balance of iron and unavoidable impurities. 
 
     
     
       10. The turbocharger turbine housing of  claim 9  comprising about 18% to about 19% chromium. 
     
     
       11. The turbocharger turbine housing of  claim 9  comprising about 4.7% to about 5.3% nickel. 
     
     
       12. The turbocharger turbine housing of  claim 9  comprising about 0.9% to about 1.1% tungsten. 
     
     
       13. The turbocharger turbine housing of  claim 9  comprising about 0.43% to about 0.47% carbon. 
     
     
       14. A method of fabricating a turbocharger turbine housing, the method comprising the step of:
 forming the turbocharger turbine housing from an austenitic stainless steel alloy, wherein the austenitic stainless steel alloy comprises, by weight: 
 about 16% to about 21% chromium; 
 about 4.5% to about 5.5% nickel; 
 3% to 4% manganese; 
 1.3% to 1.7% silicon; 
 about 0.8% to about 1.2% tungsten; 
 0.5% to 0.7% molybdenum; 
 0.45% to 0.55% niobium; 
 about 0.4% to about 0.5% carbon; 
 about 0.03% phosphorous or less; 
 about 0.03% sulfur or less; 
 about 0.01 to about 0.15% nitrogen; and 
 a balance of iron and unavoidable impurities.

Cited by (0)

No later patents cite this yet.

References (0)

No backward citations on record.